Dynamic Loads and Structural Criteria
Final rept. Nov 1973-Oct 1974
TECHNOLOGY INC DAYTON OH
Pagination or Media Count:
Preparatory to developing mission profiles for future attack, crane, observation, assault, transport, and utility helicopters, the flight condition recognition FCR technique was applied to some 10-hour data samples for each of the following class-model helicopters which had acquired 200 or more hours of multichannel oscillograph data during operational usage surveys while the helicopters operated under combat conditions in Southeast Asia SEA attack - AH-1G, crane - CH-54A, observation - OH-6A, assault - UH-1H, transport - CH-47A, and utility - UH-1H.